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执行固定翼一级性能校核（巡航所需推力、爬升率/余度）。当总体闭环需要性能判据或要定位性能不满足原因时调用。
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| name | fixed_wing_performance_runbook |
| description | 执行固定翼一级性能校核（巡航所需推力、爬升率/余度）。当总体闭环需要性能判据或要定位性能不满足原因时调用。 |
| stage | class2_preliminary |
| code_module | aircraft_design/class2_preliminary/performance.py |
| dependencies | ["fixed_wing_performance_spec"] |
fixed_wing_overall_sizing_runbook 闭环驱动，不建议作为独立入口。initial_guess.thrust_to_weight、initial_guess.wing_loading_painitial_guess.cd0、initial_guess.oswald_e、initial_guess.aspect_ratiorequirements.cruise_altitude_m、requirements.cruise_machdesign_data.json.outputs.mtow_kg、wing_area_m2 等）cruise_required_thrust_n：巡航点阻力对应的所需推力climb_rate_m_s：基于推力等级与阻力模型的一级爬升率估算cd0 或提高 e/AR，其次提高推重比或降低重量thrust_to_weight，其次降低重量/阻力（cd0、e）